Model: 1386M88P04

Aircraft Turbine Nozzle Support

Properties:

Inside Diameter
3.126 inches
Overall Length
Between 2.465 inches and 2.469 inches
Outside Diameter
Between 33.550 inches and 33.570 inches
Mounting Hole Diameter
Between 0.274 inches and 0.283 inches
Mounting Hole Quantity
79
End Application
Aircraft eng f110g129
Criticality Code Justification
Agav
Material
Steel
NSN
2840-01-307-6359
Part Number
1386M88P04
Description
Support,turbine Nozzle,aircraft
CAGE
07482

A support used for a nozzle,turbine,aircraft gas turbine engine.

Part 1386M88P04 NSN 2840-01-307-6359

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
51909
FIIG:
A521B0
Concept No.:
1
App. Key:
Cond. Code:
1
Status:
A

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
ESD:
MMAC:
PR
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
41.0 X 41.0 X 4.8
Paclk Weight:
25.0000lbs
Item Weight:
15.0000lbs
Item Dim:
034003400040
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F011909214
SPI Rev.:
B
SPC Mkg:
ZZ
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
WCC:
671
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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Schedule B and Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft

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